Click here to make tpub.com your Home Page

Page Title: Table I. Maximum null voltages.
Back | Up | Next

Click here for thousands of PDF manuals

Google


Web
www.tpub.com

Home

   
Information Categories
.... Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion
   
   

 




img
MIL-S-48461B(AR)
3 . 3 . 3 Rotor voltages at null. The maximum rms value for all voltage
c o m p o n e n t s shall be as specified for each item of table I after the assembly
h a s been rotated about the roll axis to the position which reduces the
i n - p h a s e component of the measured output voltage to a minimum value. (See
4.6.2.3)
TABLE I. Maximum null voltages.
3.3.4 Spurius signal components. There shall be no periodic signal
E
E
components of EAC, EB C ,  E H , and JM with the exception of the 400 Hz
s i g n a l voltage and harmonics of the 400 Hz signal voltage. (See 4 . 6 . 2 . 4 )
3 . 3 . 5 S e t t l i n g t i m e .  T h e assembly output voltages shall attain steady
s t a t e within one second of a 15 degree displacement of the roll axis. The
d i s p l a c e m e n t rate shall be not less than 150 degrees per second. (See 4.6.2.5)
3 . 4 S e a l i n g .  W i t h an internal nitrogen pressure of 5.0 + 0.1 pounds per
s q u a r e inch gauge (psig), the assembly shall exhibit a pressure drop not
g r e a t e r than 0.2 psig for not less than 2 hours. The pressurized assembly
s h a l l be purged with dry nitrogen in accordance with BB-N-411, type I, grade
B , class 1 with a dewpoint of -25F or lower and shall have a final pressure
o f 0.0 + 0.2, -0.0 psig. ( S e e 4 . 6 . 4 )
3.5 E n v i r o n m e n t a l .
3 . 5 . 1 S h o c k . The assembly shall be capable of operating as specified
h e r e i n after exposure under the conditions of 3.1.3 to three half sine wave
s h o c k pulses of 40 + 4 gravity unit (g) for a duration of 18 + 3 milliseconds
( m s e c ) applied in each direction along three mutually perpendicular axes. In
a d d i t i o n , the assembly shall be capable of withstanding three half sine wave
s h o c k pulses of 100.0 + 10.0 g for a duration fo 1.5 + 0.2 msec applied in
each direction along three mutually perpendicular axes. (See 4.6.3.1)
7

Privacy Statement - Press Release - Copyright Information. - Contact Us

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business